GB201804900D0 - Actuation control system - Google Patents
Actuation control systemInfo
- Publication number
- GB201804900D0 GB201804900D0 GBGB1804900.7A GB201804900A GB201804900D0 GB 201804900 D0 GB201804900 D0 GB 201804900D0 GB 201804900 A GB201804900 A GB 201804900A GB 201804900 D0 GB201804900 D0 GB 201804900D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- control system
- actuation control
- actuation
- control
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Safety Devices In Control Systems (AREA)
- Retarders (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/083,826 US8583294B2 (en) | 2011-04-11 | 2011-04-11 | Actuation control system |
GB1206403.6A GB2490032B (en) | 2011-04-11 | 2012-04-11 | Actuation control system |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201804900D0 true GB201804900D0 (en) | 2018-05-09 |
GB2560266A GB2560266A (en) | 2018-09-05 |
GB2560266B GB2560266B (en) | 2018-11-28 |
Family
ID=46177169
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1206403.6A Active GB2490032B (en) | 2011-04-11 | 2012-04-11 | Actuation control system |
GB1804900.7A Active GB2560266B (en) | 2011-04-11 | 2012-04-11 | Actuation control system |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1206403.6A Active GB2490032B (en) | 2011-04-11 | 2012-04-11 | Actuation control system |
Country Status (2)
Country | Link |
---|---|
US (1) | US8583294B2 (en) |
GB (2) | GB2490032B (en) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10191127B2 (en) | 2012-10-31 | 2019-01-29 | Aspect Imaging Ltd. | Magnetic resonance imaging system including a protective cover and a camera |
US10794975B2 (en) | 2010-09-16 | 2020-10-06 | Aspect Imaging Ltd. | RF shielding channel in MRI-incubator's closure assembly |
US9316112B2 (en) * | 2011-12-21 | 2016-04-19 | Rohr, Inc. | Variable area fan nozzle with drive system health monitoring |
US20140300469A1 (en) * | 2013-04-09 | 2014-10-09 | Aspect Imaging Ltd. | Multi-fault detecting and alerting system |
FR3010387B1 (en) * | 2013-09-10 | 2015-10-09 | Airbus Operations Sas | AIRCRAFT COMPRISING A DEVICE FOR CONTROLLING A VARIABLE SECTION TUBE SUPPLIED BY TWO INDEPENDENT ELECTRICAL SUPPLIES |
DE202013105212U1 (en) | 2013-11-17 | 2013-12-19 | Aspect Imaging Ltd. | Locking device of an MRI incubator |
US9860304B2 (en) * | 2014-01-21 | 2018-01-02 | Woodward, Inc. | Redundant CAN interface for dual actuation systems |
US10570936B2 (en) * | 2014-03-07 | 2020-02-25 | Parker-Hannifin Corporation | Symmetrically loaded dual hydraulic fly-by-wire actuator |
US9382011B2 (en) * | 2014-04-10 | 2016-07-05 | Pratt & Whitney Canada Corp. | Multiple aircraft engine control system and method of communicating data therein |
US10180076B2 (en) | 2015-06-01 | 2019-01-15 | Hamilton Sundstrand Corporation | Redundant speed summing actuators |
EP3130539B1 (en) * | 2015-08-12 | 2020-04-08 | Rolls-Royce North American Technologies, Inc. | Heat exchanger for a gas turbine engine propulsion system |
FR3045013B1 (en) * | 2015-12-14 | 2019-05-17 | Safran Nacelles | HYDRAULIC CONTROL SYSTEM FOR A THRUST INVERTER COMPRISING A DATA CONCENTRATING MODULE |
US11988730B2 (en) | 2016-08-08 | 2024-05-21 | Aspect Imaging Ltd. | Device, system and method for obtaining a magnetic measurement with permanent magnets |
US11399732B2 (en) | 2016-09-12 | 2022-08-02 | Aspect Imaging Ltd. | RF coil assembly with a head opening and isolation channel |
EP3500486B1 (en) * | 2017-02-01 | 2022-08-03 | Thales Canada Inc. | Backup actuation control unit for controlling an actuator dedicated to a given surface and method of using same |
DE102018207141A1 (en) | 2018-05-08 | 2019-11-14 | Zf Friedrichshafen Ag | System for controlling an electromechanical actuator for individually setting a collective offset for a helicopter |
US10816070B2 (en) | 2018-09-26 | 2020-10-27 | Woodward, Inc. | Geared rotary power distribution unit with mechanical differential gearing for multiple actuator systems |
CN109343335A (en) * | 2018-11-05 | 2019-02-15 | 中国航空工业集团公司西安飞机设计研究所 | A kind of hatch door redundance control system |
RU2744587C1 (en) * | 2020-06-03 | 2021-03-11 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Fail-safe electromechanical control system for reversing device of gas turbine engine |
RU2757744C1 (en) * | 2020-06-08 | 2021-10-21 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Electromechanical control system for the reversing device of a gas turbine engine with highly reliable power supply |
RU2757949C1 (en) * | 2020-06-08 | 2021-10-25 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Electromechanical system for controlling the reverser apparatus of a gas turbine engine |
US11987344B2 (en) * | 2020-07-13 | 2024-05-21 | Embraer S.A. | Rudder system architecture for electrical actuators |
US11787528B2 (en) * | 2020-12-23 | 2023-10-17 | Whippany Actuation Systems Llc | Jam free dual-redundant actuator lane changer system and process |
US11796990B2 (en) | 2021-08-24 | 2023-10-24 | Woodward, Inc. | Model based monitoring of faults in electro-hydraulic valves |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4035705A (en) | 1975-03-17 | 1977-07-12 | Sperry Rand Corporation | Fail-safe dual channel automatic pilot with maneuver limiting |
US4159444A (en) | 1978-03-21 | 1979-06-26 | Sperry Rand Corporation | Fail operational dual electromechanical servo actuator for aircraft with model monitoring |
US4594537A (en) * | 1983-12-27 | 1986-06-10 | United Technologies Corporation | Redundant control system for X-wing valve actuators |
US4800798A (en) | 1984-12-11 | 1989-01-31 | The United States Of America As Represented By The Secretary Of The Air Force | Control surface dual redundant servomechanism |
US5206810A (en) * | 1991-02-07 | 1993-04-27 | General Electric Company | Redundant actuator control |
IL115248A (en) * | 1994-09-29 | 2000-07-16 | Gen Electric | Hydraulic failsafe system and method for an axisymmetric vectoring nozzle |
US6195247B1 (en) * | 1998-06-02 | 2001-02-27 | Pratt & Whitney Canada | Exciter controlled by FADEC system |
FR2846375B1 (en) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | ELECTROMACANIC PUSH INVERTER FOR TURBOREACTOR WITH RELEASE OF DOOR MOVEMENT |
FR2846377B1 (en) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | ELECTROMECHANICAL THRUST INVERTER FOR PERMANENTLY POSITION CONTROLLED TURBOREACTOR |
US7021587B1 (en) | 2004-01-07 | 2006-04-04 | Trutrak Flight Systems, Inc | Dual channel fail-safe system and method for adjusting aircraft trim |
US8260492B2 (en) | 2005-08-05 | 2012-09-04 | Honeywell International Inc. | Method and system for redundancy management of distributed and recoverable digital control system |
GB0706270D0 (en) | 2007-03-30 | 2007-05-09 | Goodrich Actuation Systems Ltd | Actuator arrangement |
FR2927309B1 (en) | 2008-02-13 | 2010-04-16 | Aircelle Sa | CONTROL SYSTEM FOR TURBOREACTOR NACELLE |
DE102008022092A1 (en) * | 2008-05-05 | 2009-11-19 | Airbus Deutschland Gmbh | Fault-tolerant control system for adjusting the flaps of an aircraft with adjustable kinematics with a fixed axis of rotation |
GB201002315D0 (en) * | 2010-02-11 | 2010-03-31 | Goodrich Actuation Systems Ltd | Control system |
FR2963948B1 (en) | 2010-08-17 | 2014-04-25 | Snecma | DISTRIBUTED CONTROL SYSTEM FOR TURBOMACHINE |
-
2011
- 2011-04-11 US US13/083,826 patent/US8583294B2/en active Active
-
2012
- 2012-04-11 GB GB1206403.6A patent/GB2490032B/en active Active
- 2012-04-11 GB GB1804900.7A patent/GB2560266B/en active Active
Also Published As
Publication number | Publication date |
---|---|
GB201206403D0 (en) | 2012-05-23 |
US20120259483A1 (en) | 2012-10-11 |
GB2560266B (en) | 2018-11-28 |
US8583294B2 (en) | 2013-11-12 |
GB2490032B (en) | 2018-05-09 |
GB2490032A (en) | 2012-10-17 |
GB2560266A (en) | 2018-09-05 |
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